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NACA 63(2)A-015 (naca632a015-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)A-015 (naca632a015-il)
Reynolds number: 500,000
Max Cl/Cd: 72.85 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca632a015-il-500000-n5.txt
Download as CSV file: xf-naca632a015-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)A-015                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.8195   0.06447   0.06123  -0.0533   1.0000   0.0082
 -14.250  -0.8588   0.05607   0.05251  -0.0566   1.0000   0.0082
 -14.000  -0.8830   0.05038   0.04654  -0.0578   1.0000   0.0082
 -13.750  -0.8939   0.04674   0.04275  -0.0580   1.0000   0.0081
 -13.500  -0.9084   0.04272   0.03845  -0.0575   1.0000   0.0082
 -13.250  -0.9160   0.03962   0.03509  -0.0566   1.0000   0.0084
 -13.000  -0.9187   0.03721   0.03251  -0.0554   1.0000   0.0084
 -12.750  -0.9180   0.03519   0.03030  -0.0540   1.0000   0.0084
 -12.500  -0.9162   0.03331   0.02826  -0.0523   1.0000   0.0085
 -12.250  -0.9151   0.03142   0.02622  -0.0504   1.0000   0.0085
 -12.000  -0.9120   0.02984   0.02453  -0.0483   1.0000   0.0087
 -11.750  -0.9051   0.02877   0.02340  -0.0464   1.0000   0.0088
 -11.500  -0.8980   0.02765   0.02219  -0.0442   1.0000   0.0090
 -11.250  -0.8906   0.02644   0.02087  -0.0419   1.0000   0.0090
 -11.000  -0.8819   0.02558   0.01994  -0.0395   1.0000   0.0091
 -10.750  -0.8735   0.02471   0.01899  -0.0369   1.0000   0.0092
 -10.500  -0.8651   0.02399   0.01821  -0.0341   1.0000   0.0095
 -10.250  -0.8581   0.02317   0.01732  -0.0310   1.0000   0.0094
 -10.000  -0.8524   0.02256   0.01664  -0.0274   1.0000   0.0096
  -9.750  -0.8257   0.02149   0.01547  -0.0281   0.9920   0.0098
  -9.500  -0.7979   0.02057   0.01446  -0.0289   0.9826   0.0101
  -9.250  -0.7679   0.01968   0.01347  -0.0301   0.9710   0.0104
  -9.000  -0.7326   0.01877   0.01246  -0.0324   0.9588   0.0106
  -8.750  -0.6937   0.01780   0.01142  -0.0356   0.9451   0.0112
  -8.500  -0.6527   0.01693   0.01050  -0.0391   0.9299   0.0117
  -8.250  -0.6147   0.01627   0.00975  -0.0419   0.9102   0.0123
  -8.000  -0.5888   0.01577   0.00913  -0.0419   0.8865   0.0127
  -7.750  -0.5693   0.01534   0.00856  -0.0405   0.8628   0.0132
  -7.500  -0.5519   0.01493   0.00804  -0.0387   0.8433   0.0136
  -7.250  -0.5343   0.01456   0.00758  -0.0369   0.8270   0.0140
  -7.000  -0.5158   0.01423   0.00718  -0.0352   0.8130   0.0145
  -6.750  -0.4965   0.01393   0.00680  -0.0337   0.8007   0.0154
  -6.500  -0.4771   0.01363   0.00640  -0.0321   0.7897   0.0161
  -6.250  -0.4566   0.01334   0.00608  -0.0308   0.7798   0.0172
  -6.000  -0.4353   0.01311   0.00580  -0.0296   0.7709   0.0188
  -5.750  -0.4134   0.01288   0.00554  -0.0285   0.7617   0.0205
  -5.500  -0.3910   0.01267   0.00528  -0.0275   0.7537   0.0228
  -5.250  -0.3682   0.01246   0.00505  -0.0265   0.7454   0.0252
  -5.000  -0.3449   0.01229   0.00481  -0.0256   0.7379   0.0278
  -4.750  -0.3218   0.01208   0.00459  -0.0248   0.7296   0.0302
  -4.500  -0.2979   0.01194   0.00439  -0.0240   0.7220   0.0329
  -4.250  -0.2745   0.01172   0.00418  -0.0232   0.7141   0.0353
  -4.000  -0.2505   0.01157   0.00397  -0.0225   0.7065   0.0376
  -3.750  -0.2263   0.01139   0.00376  -0.0217   0.6994   0.0397
  -3.500  -0.2022   0.01123   0.00358  -0.0210   0.6916   0.0430
  -3.250  -0.1776   0.01108   0.00340  -0.0204   0.6845   0.0464
  -3.000  -0.1532   0.01091   0.00323  -0.0197   0.6769   0.0508
  -2.750  -0.1286   0.01077   0.00306  -0.0191   0.6704   0.0559
  -2.500  -0.1039   0.01060   0.00291  -0.0185   0.6632   0.0653
  -2.250  -0.0800   0.01041   0.00275  -0.0177   0.6561   0.0867
  -2.000  -0.0681   0.00931   0.00232  -0.0151   0.6495   0.2881
  -1.750  -0.0562   0.00838   0.00207  -0.0123   0.6428   0.4705
  -1.500  -0.0333   0.00819   0.00201  -0.0113   0.6364   0.5189
  -1.250  -0.0088   0.00807   0.00197  -0.0106   0.6294   0.5512
  -1.000   0.0153   0.00799   0.00193  -0.0098   0.6216   0.5777
  -0.750   0.0397   0.00792   0.00191  -0.0090   0.6097   0.6033
  -0.500   0.0640   0.00790   0.00190  -0.0082   0.5946   0.6245
  -0.250   0.0885   0.00790   0.00189  -0.0074   0.5801   0.6466
   0.000   0.1135   0.00791   0.00190  -0.0068   0.5699   0.6645
   0.250   0.1398   0.00791   0.00190  -0.0064   0.5605   0.6742
   0.500   0.1663   0.00795   0.00190  -0.0061   0.5510   0.6815
   0.750   0.1926   0.00798   0.00191  -0.0058   0.5414   0.6882
   1.000   0.2191   0.00801   0.00192  -0.0055   0.5330   0.6956
   1.250   0.2454   0.00807   0.00194  -0.0051   0.5236   0.7024
   1.500   0.2716   0.00810   0.00197  -0.0048   0.5134   0.7091
   1.750   0.2977   0.00817   0.00201  -0.0044   0.5032   0.7163
   2.000   0.3237   0.00822   0.00205  -0.0041   0.4929   0.7232
   2.250   0.3497   0.00828   0.00210  -0.0037   0.4827   0.7308
   2.500   0.3754   0.00836   0.00216  -0.0033   0.4714   0.7375
   2.750   0.4006   0.00844   0.00222  -0.0028   0.4575   0.7450
   3.250   0.4501   0.00865   0.00238  -0.0016   0.4246   0.7605
   3.500   0.4746   0.00879   0.00248  -0.0010   0.4066   0.7688
   3.750   0.4983   0.00893   0.00259  -0.0003   0.3857   0.7771
   4.250   0.5429   0.00937   0.00289   0.0017   0.3347   0.7961
   4.500   0.5647   0.00961   0.00307   0.0027   0.3130   0.8067
   4.750   0.5871   0.00982   0.00325   0.0037   0.2954   0.8183
   5.000   0.6093   0.01003   0.00346   0.0047   0.2786   0.8308
   5.250   0.6311   0.01026   0.00367   0.0057   0.2615   0.8448
   5.500   0.6531   0.01050   0.00389   0.0067   0.2456   0.8600
   5.750   0.6761   0.01072   0.00412   0.0074   0.2335   0.8769
   6.000   0.7021   0.01092   0.00436   0.0076   0.2245   0.8950
   6.250   0.7313   0.01117   0.00463   0.0070   0.2155   0.9133
   6.500   0.7647   0.01145   0.00492   0.0055   0.2070   0.9288
   6.750   0.8002   0.01175   0.00523   0.0035   0.1993   0.9416
   7.000   0.8369   0.01210   0.00556   0.0011   0.1899   0.9518
   7.250   0.8728   0.01239   0.00587  -0.0010   0.1832   0.9603
   7.500   0.9064   0.01273   0.00619  -0.0028   0.1754   0.9685
   7.750   0.9394   0.01304   0.00652  -0.0043   0.1683   0.9750
   8.250   1.0000   0.01373   0.00720  -0.0064   0.1524   0.9895
   8.500   1.0301   0.01414   0.00758  -0.0075   0.1441   0.9968
   8.750   1.0581   0.01458   0.00798  -0.0082   0.1322   1.0000
   9.000   1.0698   0.01491   0.00829  -0.0055   0.1233   1.0000
   9.250   1.0798   0.01530   0.00865  -0.0025   0.1139   1.0000
   9.500   1.0861   0.01570   0.00900   0.0012   0.1058   1.0000
   9.750   1.0935   0.01610   0.00939   0.0047   0.0983   1.0000
  10.000   1.1014   0.01657   0.00985   0.0079   0.0912   1.0000
  10.250   1.1105   0.01709   0.01036   0.0107   0.0850   1.0000
  10.500   1.1209   0.01763   0.01090   0.0131   0.0794   1.0000
  10.750   1.1304   0.01826   0.01153   0.0156   0.0735   1.0000
  11.000   1.1413   0.01890   0.01218   0.0176   0.0684   1.0000
  11.500   1.1612   0.02042   0.01372   0.0215   0.0588   1.0000
  11.750   1.1706   0.02131   0.01462   0.0233   0.0550   1.0000
  12.000   1.1812   0.02218   0.01552   0.0247   0.0521   1.0000
  12.250   1.1911   0.02315   0.01652   0.0261   0.0497   1.0000
  12.500   1.1999   0.02426   0.01767   0.0275   0.0474   1.0000
  12.750   1.2102   0.02532   0.01878   0.0286   0.0458   1.0000
  13.000   1.2197   0.02647   0.02000   0.0296   0.0440   1.0000
  13.250   1.2281   0.02777   0.02134   0.0305   0.0424   1.0000
  13.500   1.2347   0.02925   0.02286   0.0314   0.0408   1.0000
  13.750   1.2419   0.03073   0.02441   0.0321   0.0395   1.0000
  14.000   1.2504   0.03216   0.02593   0.0327   0.0382   1.0000
  14.250   1.2570   0.03377   0.02761   0.0333   0.0368   1.0000
  14.500   1.2620   0.03559   0.02949   0.0337   0.0353   1.0000
  14.750   1.2650   0.03764   0.03159   0.0341   0.0341   1.0000
  15.000   1.2699   0.03956   0.03359   0.0343   0.0330   1.0000
  15.250   1.2740   0.04161   0.03574   0.0344   0.0320   1.0000
  15.500   1.2770   0.04384   0.03805   0.0344   0.0311   1.0000
  15.750   1.2782   0.04632   0.04060   0.0343   0.0302   1.0000
  16.000   1.2780   0.04903   0.04338   0.0340   0.0295   1.0000
  16.250   1.2764   0.05200   0.04642   0.0336   0.0286   1.0000
  16.500   1.2754   0.05497   0.04949   0.0330   0.0281   1.0000
  16.750   1.2735   0.05813   0.05275   0.0323   0.0276   1.0000
  17.000   1.2707   0.06148   0.05620   0.0315   0.0270   1.0000
  17.250   1.2661   0.06514   0.05996   0.0304   0.0266   1.0000
  17.500   1.2611   0.06892   0.06384   0.0293   0.0261   1.0000
  17.750   1.2549   0.07295   0.06796   0.0280   0.0257   1.0000
  18.000   1.2461   0.07745   0.07255   0.0264   0.0253   1.0000
  18.250   1.2362   0.08219   0.07739   0.0246   0.0251   1.0000
  18.500   1.2254   0.08713   0.08242   0.0227   0.0247   1.0000
  18.750   1.2120   0.09258   0.08796   0.0205   0.0243   1.0000
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